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首页> 外文期刊>International Journal of Heat and Fluid Flow >A comparison of laminar-turbulent boundary-layer transitions induced by deterministic and random oblique waves at Mach 3
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A comparison of laminar-turbulent boundary-layer transitions induced by deterministic and random oblique waves at Mach 3

机译:确定性和随机斜波在3马赫处引起的层流湍流边界层过渡的比较

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A numerical investigation of transition processes initiated by deterministic and random disturbances is presented for a Mach 3 flat-plate boundary layer. In both cases, disturbance forcing is localized slightly downstream of the leading edge of the flat plate. The targeted kind of disturbance for laminar-turbulent transitions is an oblique wave but it is introduced with two different ways: deterministic suction and blowing at the wall, or random volume forcing at the edge of the boundary layer. Moreover, the forced perturbations are sinusoidal in spanwise direction with a single fixed wavenumber in the deterministic case and multiple harmonics in the random case. In the latter case, the random disturbance evolution is characterized by the RMS values of Fourier transformed velocities in a band of frequency to cover the amplifications of multiple frequency components. The observed path to turbulence with respect to the two cases are compared in three stages: linear stage, non-linear regime, and breakdown to turbulence. In the initial stage, the amplitude of unsteady disturbances grows exponentially due to a linear instability of the boundary layer, as it could be observed in the deterministic forcing case. This exponential growth is also observed after considering a broad band of frequencies in the random forcing case. In the second stage, non-linearity leads to the formation of streamwise streaks via the lift-up effect. In the deterministic case, these streaks are steady, while they take the form of low-frequency traveling waves in the case of random forcing. However, in the random forcing case a streak instability could not clearly be identified. In the final stage, sudden breakdown to turbulence occurs at a fixed streamwise location in the deterministic case, marked by a sharp rise in skin friction. Non-periodicities appear only downstream of the breakdown location. In the random forcing case, breakdown takes place within a transition zone in which one can observe the formation of distinct turbulent spots. (C) 2015 Elsevier Inc. All rights reserved.
机译:对马赫3平板边界层提出了由确定性和随机扰动引发的过渡过程的数值研究。在这两种情况下,干扰强迫都位于平板前缘的稍下游。层流湍流过渡的目标扰动是斜波,但它以两种不同的方式引入:确定性的吸力和在壁上的吹动,或在边界层边缘的随机体积强迫。此外,在确定性情况下,强制扰动在翼展方向上为正弦波,具有单个固定波数,在随机情况下,具有多个谐波。在后一种情况下,随机扰动演变的特征是在一个频带内进行傅立叶变换速度的RMS值,以覆盖多个频率分量的放大倍数。在三个阶段中比较了两种情况下观察到的湍流路径:线性阶段,非线性状态和湍流分解。在初始阶段,非稳定扰动的幅度由于边界层的线性不稳定性而呈指数增长,正如在确定性强迫情况下所观察到的那样。在考虑随机强迫情况下的宽频带后,也观察到这种指数增长。在第二阶段,非线性通过提起效应导致形成流状条纹。在确定性情况下,这些条纹是稳定的,而在随机强迫的情况下,它们以低频行波的形式出现。但是,在随机强迫的情况下,条纹不稳定性不能清楚地识别出来。在最后阶段,在确定性情况下,在固定的水流位置突然发生湍流破坏,其特征是皮肤摩擦力急剧上升。非周期性仅出现在故障位置的下游。在随机强迫情况下,击穿发生在过渡区内,在该过渡区内,可以观察到明显的湍流斑的形成。 (C)2015 Elsevier Inc.保留所有权利。

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